View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 14066.55710725 -.00000006 00000-0 30563-4 0 3258
2 24278 098.5201 094.4163 0350456 201.1686 283.7738 13.53016919866921
| Epoch (UTC): | 07 March 2014 13:22:14 |
| Eccentricity: | 0.0350456 |
| inclination: | 98.5201° |
| perigee height: | 800 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 94.4163° |
| argument of perigee: | 201.1686° |
| revolutions per day: | 13.53016919 |
| mean anomaly at epoch: | 283.7738° |
| orbit number at epoch: | 86692 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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